CN112758352B

CN112758352B - Auxiliary pulling device for rocket launcher

Info

Publication number: CN112758352B
Application number: CN202011596706.0A
Authority: CN
Inventors: 周龙; 王寿军; 兰公英; 高鹏; 全金; 胡小伟; 雷理军; 豆旭安; 杨毅强
Original assignee: Beijing Zhongke Aerospace Technology Co Ltd
Current assignee: Beijing Zhongke Aerospace Technology Co Ltd
Priority date: 2020-12-29
Filing date: 2020-12-29
Publication date: 2022-05-24
Anticipated expiration: 2040-12-29
Also published as: CN112758352A

Abstract

The application discloses an auxiliary pulling device for a rocket launcher, which comprises two supporting pieces and two traction ropes; the two supporting pieces are respectively positioned at two sides of the plug, the first ends of the two supporting pieces are respectively connected with the vertical frame, and the second ends of the two supporting pieces respectively extend to be higher than the plug; the extending directions of the two supporting pieces are parallel to the longitudinal central axis of the rocket; one ends of the two traction ropes are respectively connected with the second ends of the two supporting pieces, and the other ends of the two traction ropes are connected with the release plug; before the rocket is launched, the vertical frame is separated from the plug under the condition of inclining relative to the rocket body of the rocket; the two traction ropes pull the inserting and removing movement to the vertical frame, and when the inserting and removing movement is contacted with the vertical frame, the lowest point is higher than the emission supporting part. This application can be drawn rope control motion route when taking off to insert and drop to can take off the accurate control and insert the route that drops, prevent that cable and transmission support component from interfering, make the cable drop to the assigned position smoothly, the cable of being convenient for is retrieved.

Description

Auxiliary pulling device for rocket launching cradle

Technical Field

The application relates to the technical field of aerospace, in particular to an auxiliary pulling device for a rocket launcher.

Background

Before the rocket is launched, a boosting carrier launching support system is needed to carry out early-stage transportation, support and the like. The launch support system of the booster vehicle comprises a vertical frame and a power supply device, wherein the vertical frame is mainly used for supporting the bottom of the rocket before the rocket is launched, preventing the rocket from toppling and enabling the rocket to maintain a launching posture. The power supply equipment is used for providing electric energy for the rocket when the rocket is launched. Before the rocket is launched to the sky, the power supply equipment provides electric energy for the rocket body through a cable, and when the rocket is ready to take off to the sky, the cable needs to be separated from the rocket body. Specifically, a plug is arranged on an rocket body of the rocket, a first end of the cable is connected with a release plug, and a second end of the cable is connected with the erecting frame. When the arrow body is provided with electric energy, the inserting and releasing device is inserted on the plug.

At present, the way of disengaging the cable and the arrow body is as follows: a hydraulic winch is arranged on the vertical frame, then a separation steel wire rope is arranged, the first end of the separation steel wire rope is connected with the release and insertion device, and the second end of the separation steel wire rope is connected with the hydraulic winch. When the disengaging and inserting needs to be separated from the plug on the arrow body, the disengaging and inserting automatic electric disengaging is firstly performed, power supply is stopped, then the hydraulic winch starts to rotate, the separation steel wire rope is driven to be recycled, and the disengagement and inserting are driven by the separation steel wire rope to fall off from the plug.

However, in the above manner of disengaging the cable from the arrow body, the separation steel wire rope drives the disengaging and inserting to disengage, the disengaging and inserting downward falling process is a free falling process, and the path of the disengaging and inserting free falling process cannot be controlled, so that the disengaging and inserting falling process is easily interfered with other components such as the uniform-load dragging seat and the clamp on the vertical frame, and also easily interfered with the guide component of the separation steel wire rope, so that the cable cannot be recovered to the specified position.

Disclosure of Invention

The utility model aims at providing an auxiliary take-off device for rocket mount can control and take off the route of inserting and the fall after the plug separation, reduces the cable and all carry the risk that launching support parts such as bracket and clamp interfered for the cable can be retrieved smoothly.

The application provides an auxiliary pulling device for a rocket launcher, wherein the rocket launcher comprises a vertical frame and a cable, one end of the cable is connected with the vertical frame, the other end of the cable is provided with a pulling-inserting piece, the vertical frame is supported at the bottom of a rocket, a plug is arranged on a rocket body of the rocket, and the pulling-inserting piece is inserted into the plug; the erecting frame is provided with a launching support part; the auxiliary stripping device for the rocket launcher comprises: two supporting pieces and two traction ropes; the two supporting pieces are respectively positioned at two sides of the plug, first ends of the two supporting pieces are respectively connected with the vertical frame, and second ends of the two supporting pieces respectively extend to be higher than the plug; the extending directions of the two supporting pieces are parallel to the longitudinal central axis of the rocket; two ends of one of the traction ropes are respectively connected with the second end of one of the supporting pieces and the release plug, and two ends of the other traction rope are respectively connected with the second end of the other of the supporting pieces and the release plug; the disengaging is disengaged from the plug in the event that the erector is tilted relative to the rocket body of the rocket prior to launch of the rocket; the two traction ropes draw the inserting and removing movement to the vertical frame, and when the inserting and removing movement is in contact with the vertical frame, the lowest point is higher than the emission supporting part.

Optionally, the two supporting members are symmetrically distributed on two sides of the plug, the lengths of the two pulling ropes are equal, so that the circle center of the circle is the midpoint of a connecting line of the second ends of the two supporting members, and the disengaging and inserting trajectory is located on the plane where the central axis of the rocket and the plug are located.

Optionally, the auxiliary pulling-off device for rocket launcher further comprises: separating the pull-cord from the drive member; the driving part is provided with a first winding drum; the driving part is arranged on the vertical frame, and two ends of the separating traction rope are respectively connected with the release insert and the first reel; after the driving component is started in the forward direction, the separation traction rope is driven to be recovered to the first winding drum, and the separation traction rope drives the separation plug to be separated from the plug.

Optionally, the auxiliary pulling-off device for rocket launcher further comprises: recovering the hauling rope, wherein the driving part is provided with a second winding drum; two ends of the recovery pulling rope are respectively connected with the release insert and the second winding drum; the driving component drives the recovery pulling rope to recover on the second winding drum after being positively started, and the recovery pulling rope is used for exerting upward acting force on the disengaging plug in the falling process after the disengaging plug and the plug are separated.

Optionally, before the rocket is launched, in a case where the erector is horizontal with respect to the rocket body of the rocket from an inclined position, the driving unit is reversely actuated to extend the separation towline and the recovery towline.

Optionally, a first distance is provided between the first winding drum and the release and insertion, a second distance is provided between the second winding drum and the release and insertion, and the first distance is smaller than the second distance.

Optionally, the drive component comprises a primary drive and a backup drive; in the event of a failure of the primary drive, the backup drive is activated.

Optionally, a value range of the angle a of the vertical frame inclined relative to the rocket body of the rocket includes: a is more than or equal to 15 degrees and more than or equal to 9 degrees; the separation pulling force applied by the separation pulling rope to the disengaging and inserting has a first direction, the extension line of the central axis of the plug and the disengaging and inserting is a disengaging and inserting axis, and the angle deviation between the first direction and the disengaging and inserting axis is less than 5 degrees; when the plug and the socket are connected, the angular deviation between the cable and the plug axis is 40 degrees or less.

Optionally, the auxiliary pulling-off device for rocket launcher further comprises: a fixing plate, a first guide, a second guide and a third guide; the fixed plate is close to the driving part, the fixed plate is arranged on the erecting frame, and the guide piece is arranged on the fixed plate; the separation pulling rope is wound on the first guide member after being stretched; the recovery traction rope is wound on the second guide member after being stretched; the cable is wound around the third guide before the rising frame is tilted.

Optionally, the number of the first guide, the second guide and the third guide is one or more than two; one end of the separation pulling rope is connected with the first winding drum after passing through one or more than two first guide pieces, and one end of the recovery pulling rope is connected with the second winding drum after passing through one or more than two second guide pieces; one end of the cable passes through one or more than two third guide pieces and then is connected with the plug-in and plug-out connector

This application is through setting up two support piece to make the top of two support piece be higher than the position of taking off the insertion, then connect the one end of two tractive lines and the top of two support piece, the other end of two tractive lines with take off the insertion and connect. Therefore, when the disengaging and inserting piece falls downwards, the running path can be controlled by the pulling rope, specifically, circular motion can be carried out by taking a point on a connecting line between the top ends of the two supporting pieces as a circle center and taking the distance between the circle center and the disengaging and inserting piece as a radius. That is, the two support members and the two pull cords control the drop path of the release insertion to be one circle. The lowest point of the circumference is higher than the emission supporting part, so that the falling path of the plug can be accurately controlled, the plug and the cable are prevented from interfering with the emission supporting part, the cable can smoothly fall to a specified position, and the cable is convenient to recycle.

Drawings

FIG. 1 is a schematic view of a vertical state of a riser of an auxiliary pulling apparatus for a rocket launcher according to an embodiment of the present application;

FIG. 2 is a schematic view of the inclined state of the riser of the auxiliary pulling-off device for rocket launcher provided by the embodiment of the present application;

FIG. 3 is a schematic view of a riser of an auxiliary pulling apparatus for a rocket launcher according to an embodiment of the present application;

fig. 4 is a schematic diagram illustrating a disengaging and dropping path of an auxiliary disengaging device for a rocket launcher according to an embodiment of the present application.

Description of the reference numerals

Rocket 100, riser 110, cable 120, plug 130, launch support member 140, eyebolt 150, support member 200, pull rope 210, breakaway pull rope 220, drive member 230, first reel 240, recovery pull rope 250, second reel 260, attachment plate 270, first guide 280, second guide 290, third guide 291, breakaway insert 300, path 400.

Detailed Description

Reference will now be made in detail to the embodiments of the present application, examples of which are illustrated in the accompanying drawings, wherein like or similar reference numerals refer to the same or similar elements or elements having the same or similar function throughout. The embodiments described below with reference to the drawings are exemplary only for the purpose of explaining the present application and are not to be construed as limiting the present application.

Referring to fig. 1, a rocket 100 and a rocket 100 launcher according to an embodiment of the present invention will be described first, wherein the rocket 100 launcher includes a riser 110, cables 120, and the like, and a launch support member 140 such as a carriage and a clamp is provided on the riser 110. Before the rocket 100 is ready to be launched, the erecting frame 110 is supported at the bottom of the rocket 100, one end of a cable for supplying electric energy is connected with the erecting frame 110, the other end of the cable 120 is provided with a release plug 300, the erecting frame 110 is supported at the bottom of the rocket 100, a plug 130 is arranged on the rocket body of the rocket 100, and the release plug 300 is inserted on the plug 130.

In order to prevent the release plug 300 from being pulled out of the plug 130 and falling down during the preparation of the rocket 100, which brings the cable 120 into interference with the launching support member, the present embodiment provides an auxiliary release device for the launcher of the rocket 100, which will be described in detail below.

As shown in fig. 1 to 4, in which fig. 1 and 3 are a case where the vertical frame 110 is in a vertical state, and fig. 2 and 4 are a case where the vertical frame 110 is inclined at a certain angle, the auxiliary pulling-off device for the rocket 100 launcher provided by the embodiment of the present application includes: two support members 200 and two pull cords 210.

Wherein, the two supporting elements 200 are respectively located at two sides of the plug 130, first ends of the two supporting elements 200 are respectively connected with the vertical frame 110, and second ends of the two supporting elements 200 respectively extend to be higher than the plug 130; the two support elements 200 extend in a direction parallel to the longitudinal central axis of the rocket 100. It will be understood by those skilled in the art that the support member 200 may be provided by a member of the stand 110, or may be provided separately, and may be selected according to the actual situation. In this embodiment, two columns are preferably provided because the column 110 does not have a suitable location for securing the pull cord 210.

Specifically, both ends of one of the pulling ropes 210 are respectively connected to the second end of one of the supporting members 200 and the release plug 300, and both ends of the other pulling rope 210 are respectively connected to the second end of the other supporting member 200 and the release plug 300. Before the rocket 100 is launched, the release 300 is detached from the plug 130 under the condition that the riser 110 is inclined with respect to the rocket body of the rocket 100; the two pulling ropes 210 pull the release plug 300 to move to the rising frame 110, and the lowest point of the release plug 300 is higher than the emission support member 140 when contacting the rising frame 110. It can be seen that the two pull cords 210 can precisely control the travel path of the release 300.

In this embodiment, referring to the drawings, by providing two support members 200 such that the top ends of the two support members 200 are higher than the position of the release pin 300, one ends of two pulling cords 210 are connected to the top ends of the two support members 200, and the other ends of the two pulling cords 210 are connected to the release pin 300. Therefore, when the release pin 300 falls downward, the point on the connecting line between the top ends of the two supports 200 is used as the center of the circle, and the moving track of the release pin 300 is located on the plane where the central axis of the rocket 100 and the plug 130 are located. The release 300, i.e., the two supports 200 and the two pull cords 210 control the drop path 400 of the release 300 to be a circle. It can be understood by those skilled in the art that, in order to avoid applying an extra pulling force to the release plug 300 by the pulling rope 210 before the release plug 300 falls, the length of the pulling rope 210 is generally set to be slightly longer than the distance from the center of a circle to the release plug 300, so that in the falling process of the release plug 300, the release plug 300 is free to fall under the action of gravity, when the pulling rope 210 is straightened, the pulling rope 210 performs circular motion, and further the lowest point of the circle is set to be higher than the emission support member 140, so that the falling path 400 of the release plug 300 can be accurately controlled, the interference between the release plug 300 and the emission support member 140 by the cable 120 is prevented, the cable 120 can smoothly fall to a specified position, and the cable 120 can be conveniently recovered.

In an alternative embodiment, the two supporting elements 200 are symmetrically distributed on both sides of the plug 130, and the lengths of the two pulling ropes 210 are equal, so that the center of the circle is the midpoint of the connecting line of the second ends of the two supporting elements 200, and the trajectory of the release 300 is located on the plane where the central axis of the rocket 100 and the plug 130 are located. It will be understood by those skilled in the art that the supporting members 200 may be arranged according to the specific structure of the erecting frame 110, so that the two pulling ropes 210 can drive the release plug 300 to move on the plane of the central axis of the rocket 100 and the central axis of the two supporting members 200.

Of course, the lengths of the two supports 200 are also equal, and then the top ends of the two supports 200 are located at the same height. Plus the two pull cords 210 are equal in length. Under this condition, two pulling ropes 210 exert equal pulling force to taking off and inserting 300 for the both sides atress that takes off and inserting 300 is more even, makes to take off and inserts 300 whereabouts route 400 more accurate controllable from this to can accurately avoid launching support component 140.

In an alternative embodiment, the auxiliary releasing means for the rocket 100 launcher further comprises a release pull rope 220 and a driving member 230; the driving part 230 is provided with a first reel 240. The driving member 230 is disposed on the rising frame 110, and both ends of the separation pulling rope 220 are connected to the release sleeve 300 and the first winding reel 240, respectively. After the driving member 230 is started in the forward direction, the separation pulling rope 220 is driven to be recovered to the first reel 240, and the separation pulling rope 220 drives the release plug 300 to separate from the plug 130. It will be appreciated by those skilled in the art that the driving member 230 may be a hydraulic winch, an electric winch, a pneumatic winch, or the like, and preferably a hydraulic winch in this embodiment.

The driving part 230 is normally started, that is, the driving part 230 rotates the first reel 240 in one direction, so that the separation pulling rope 220 is wound back on the first reel 240. At this time, the anti-reverse mechanism of the driving part 230 is in a locked state to prevent the first reel 240 from being reversed, resulting in extension of the detaching cable 220, thereby affecting normal detachment of the unplug 300 and the plug 130.

After the rocket 100 is ready for launching, the driving unit 230 may be first controlled to be positively actuated so that the detaching cable 220 is gradually wound around the first reel 240, the pulling force applied to the detaching plug 300 by the detaching cable 220 is gradually increased as the detaching cable 220 is shortened, and the detaching plug 300 is detached from the plug 130 after the pulling force is greater than the coupling force between the detaching plug 300 and the plug 130.

Thus, by providing the driving member 230 and the release pulling rope 220, the release plug 300 and the plug 130 can be smoothly separated, thereby ensuring smooth launch of the rocket 100.

In an alternative embodiment, the device for assisted extraction of the launcher for rockets 100 further comprises: the traction rope 250 is recovered and the driving member 230 is provided with a second reel 260. The two ends of the recovery traction rope 250 are connected to the release 300 and the second reel 260, respectively. The driving member 230 is positively driven to drive the recovery pulling rope 250 to recover toward the second winding drum 260, and the recovery pulling rope 250 is used for applying an upward force to the socket 300 in the falling process after the socket 300 and the plug 130 are separated.

After the driving part 230 is started in the forward direction, the withdrawal string 250 is withdrawn and wound onto the second reel 260 while the withdrawal string 220 is withdrawn and wound onto the first reel 240. After the separation pulling rope 220 applies force to the release plug 300 to separate the release plug 300 from the plug 130, in the process that the release plug 300 falls downwards, the recovery pulling rope 250 applies upward force to the release plug 300, so that the release plug 300 is lifted upwards, the amplitude of the vertical swing of the cable 120 in the falling process of the release plug 300 can be reduced, and the risk of interference between the cable 120 and the emission supporting component 140 is reduced.

In addition, the pulling rope 210, the separation pulling rope 220 and the recovery pulling rope 250 work together to prevent the release 300 from rebounding, thereby reducing the risk that the release 300 and the cable 120 rebound to damage the outer circumferential surface of the rocket 100.

In one embodiment, a torque limiter is further disposed between the second reel 260 and the first reel 240 for protecting the first reel 240 from a pulling force smaller than a maximum pulling force that the release liner 300 can bear, so as to avoid damaging the plug 130 and the release liner 300 in a connected state.

In an alternative embodiment, in the case where the riser 110 is horizontal with respect to the rocket body of the rocket 100 from the inclined position before the rocket 100 is launched, the driving means 230 is actuated in reverse to extend the separation tether 220 and the recovery tether 250.

The reverse start of the driving part 230 is that the anti-reverse mechanism of the driving part 230 is unlocked, and the driving part controls the first reel 240 and the second reel 260 to rotate in the opposite direction, which is the opposite direction of the first reel 240 and the second reel 260 when the separation pulling rope 220 and the recovery pulling rope 250 are recovered. For example, when the separation pulling rope 220 and the recovery pulling rope 250 are recovered, the first reel 240 and the second reel 260 rotate clockwise, and then after the anti-reverse mechanism is unlocked, the first reel 240 and the second reel 260 rotate counterclockwise, so that the separation pulling rope 220 is released from the first reel 240 and the recovery pulling rope 250 is released from the second reel 260. Thereby restoring the length of the release cord 300 coupled to the plug 130 when the release cord 220 and the recovery cord 250 are initially released. At this point, the anti-reverse mechanism of the drive component 230 is again locked. The separation of the traction rope 220 and the recovery of the traction rope 250 back to the original length may facilitate the next use.

In an alternative embodiment, the first spool 240 has a first distance from the release insert 300 and the second spool 260 has a second distance from the release insert 300, the first distance being less than the second distance. That is, the first reel 240 has a higher height on the rising frame 110 than the second reel 260 has on the rising frame 110. Therefore, when the driving member 230 is started, the first reel 240 and the second reel 260 start to recover the detaching rope 220 and the pulling rope 250 at the same time, and the detaching rope 220 has a shorter length, so that the detaching rope 220 applies a force to the detaching plug 300 first to detach the detaching plug 300 from the plug 130; when the release plug 300 and the plug 130 are separated and then fall down, the pulling rope 210 and the recovery pulling rope 250 apply force to the release plug 300, so that the release plug 300 is lifted up, and the risk of interference between the cable 120 and the emission support member 140 is reduced. It will be understood by those skilled in the art that the first and second distances represent the lengths of the separation and

recovery lanyards

220 and 250, respectively. Specifically, in order to avoid separating the pulling rope 220 before the detachment/insertion 300 falls, recovering the pulling rope 250, and providing extra pulling force to the detachment/insertion 300 by the cable 120, it is generally configured to: the first distance is a length of the detachment traction rope 220 when fully extended, which is slightly longer than a distance between the first reel 240 and the release liner 300; the second distance is the fully extended length of the retrieval pull-cord 250, which is slightly longer than the distance between the second reel 260 and the release reel 300.

In an alternative embodiment, the drive member 230 includes a primary drive and a back-up drive; in the event of a primary drive failure, the backup drive is enabled. Therefore, when the main driving element fails, the standby driving element can also serve as a standby to drive the first winding drum 240 and the second winding drum 260 to work smoothly, so that the release and insertion 300 can be smoothly separated from the plug 130, the failure risk before the rocket 100 is launched is reduced, and the rocket 100 is ensured to be launched smoothly. It will be appreciated by those skilled in the art that the primary and backup drives may each be hydraulic, pneumatic or electric, and in this embodiment are preferably hydraulic pumps.

Generally, before the rocket 100 is launched, the erecting frame 110 will incline to a certain angle and separate from the rocket 100, so as to avoid affecting the launching of the rocket 100, and the inclined angle is generally between 9 degrees and 15 degrees, that is, the range of the angle a of the erecting frame 110 inclined relative to the rocket body of the rocket 100 includes that 15 degrees is larger than or equal to a and larger than or equal to 9 degrees. In this embodiment, in order to facilitate the separation of the release plug 300 and the plug 130, the release plug 300 and the plug 130 are designed to have a separation force not exceeding a specific value, which is 250 newtons in this embodiment. Before the release liner 300 and the plug 130 are not separated, the angle between the direction of the separation pulling force applied to the release liner 300 by the separation pulling string 220 and the axis of the release liner 300 is in a range of not more than 5 degrees.

On this premise, the separation pulling force applied to the release/insertion member 300 by the separation pulling rope 220 has a first direction, the extension line of the central axis of the plug 130 and the release/insertion member 300 is the axial direction of the release/insertion member 300, and the angular deviation between the first direction and the axial line of the release/insertion member 300 is 5 degrees or less. That is, the direction of the force applied by the separation pulling rope 220 to the release plug 300 is coincident with the axis of the release plug 300 as much as possible, so that the release plug 300 and the plug 130 can be well connected, the cable 120 can smoothly provide electric energy for the rocket 100, and the risk that the rocket 100 cannot normally supply power is reduced.

When the plug 300 and the plug 130 are connected, the angular deviation between the axes of the cable 120 and the plug 300 is 40 degrees or less. Since the bending radius is determined when the thickness and the internal structure of the cable 120 are determined, if the angle is too large, the turning radius is small, and the additional force of bending the cable 120 is applied to the position of the plug 300, so that the additional force is applied to the plug 300 during connection, which affects the connection reliability of the plug 300. Therefore, in order to avoid this, the angle setting in the present embodiment can ensure the firmness and reliability of the connection of the release/insertion member 300.

In an alternative embodiment, the assisted extraction device for a rocket 100 launcher further comprises: a fixing plate 270, a first guide 280, a second guide 290, and a third guide 291. The fixing plate 270 is adjacent to the driving part 230, the fixing plate 270 is disposed on the rising frame 110, and the guide is disposed on the fixing plate 270. After the separation pulling rope 220 is extended, it is wound around the first guide 280; after the recovery traction rope 250 is extended, it is wound around the second guide 290; the cable 120 is wound on the third guide 291 before the rising frame 110 is tilted.

Of course, it will be understood by those skilled in the art that the fixing surface of the fixing plate 270 extends in a direction parallel to the height direction of the rocket 100. Through the arrangement of the fixing plate 270, the first guide part 280, the second guide part 290 and the third guide part 291, the separation pulling rope 220, the recovery pulling rope 250 and the cable 120 can be guided in the pulling direction of the cable in the state that the rocket 100 is not inclined, and the arrangement of the guide parts has the function that the cable is placed according to a set mode when the rocket body 100 is not inclined, so that the rocket body 100 can be smoothly extended in the inclination process, and the interference condition in the inclination process is avoided.

In an alternative embodiment, the number of the first guide 280, the second guide 290 and the third guide 291 is one or more than two; one end of the separation pulling rope 220 is connected with the first reel 240 through one or more first guiding elements 280, and one end of the recovery pulling rope 250 is connected with the second reel 260 through one or more second guiding elements 290; one end of the cable 120 is connected to the release 300 through one or more third guides 291. It will be understood by those skilled in the art that the first guide 280, the second guide 290 and the third guide 291 may be provided in one or more than two, and the specific number may be determined according to the space of the installation location or the lengths of the separation pulling rope 220, the recovery pulling rope 250 and the cable 120.

The first guide 280, the second guide 290, and the third guide 291 may be plates having engaging grooves.

One end of the separation pulling rope 220 is connected to the first reel 240 through an eye screw 150 or a universal wheel fixed to the rising frame 110. The supporting point for separating the traction rope 220 is a point where the traction rope 220 is in contact with the eye screw 150 or the universal wheel. When the pull rope 220 is separated to complete the pulling work, the driven member 230 is extended and a part of its length is wound on the fixing plate 270.

It will be appreciated by those skilled in the art that in the above embodiments, the pull rope 210, the separation pull rope 220, and the recovery pull rope 250 may be steel wire rope, hemp rope with high strength, or the like. Low cost and high strength are selected criteria.

The construction, features and functions of the present application are described in detail in the embodiments illustrated in the drawings, but the present application is not limited to the embodiments illustrated in the drawings, and all equivalent embodiments modified or equivalent according to the concept of the present application are within the scope of the present application.

Claims

1. An auxiliary pulling device for a rocket launcher comprises a vertical frame and a cable, wherein one end of the cable is connected with the vertical frame, the other end of the cable is provided with a pulling-out plug, the vertical frame is supported at the bottom of a rocket, a rocket body of the rocket is provided with a plug, and the pulling-out plug is inserted into the plug; the erecting frame is provided with a launching support part; it is characterized in that the preparation method is characterized in that,

the auxiliary stripping device for the rocket launcher comprises: two supporting pieces and two traction ropes;

the two supporting pieces are respectively positioned at two sides of the plug, first ends of the two supporting pieces are respectively connected with the vertical frame, and second ends of the two supporting pieces respectively extend to be higher than the plug; the extending directions of the two supporting pieces are parallel to the longitudinal central axis of the rocket;

two ends of one of the traction ropes are respectively connected with the second end of one of the supporting pieces and the release plug, and two ends of the other traction rope are respectively connected with the second end of the other of the supporting pieces and the release plug;

the disengaging is disengaged from the plug in the event that the erector is tilted relative to the rocket body of the rocket prior to launch of the rocket; the two traction ropes draw the inserting and extracting movement to move to the vertical frame, and when the inserting and extracting movement is contacted with the vertical frame, the lowest point is higher than the launching support part;

The auxiliary pulling-off device for the rocket launcher further comprises: separating the pull-cord from the drive member; the driving part is provided with a first winding drum;

the driving part is arranged on the vertical frame, and two ends of the separating traction rope are respectively connected with the release insert and the first reel;

after the driving component is started in the forward direction, the separation traction rope is driven to be recovered to the first winding drum, and the separation traction rope drives the separation plug to be separated from the plug.

2. An auxiliary releasing device for a rocket launcher according to claim 1, wherein two supporting members are symmetrically distributed on both sides of said plug, and the lengths of the two pulling ropes are equal, so that the center of the circle is the midpoint of the connecting line of the second ends of the two supporting members, wherein the dropping path of the two supporting members and the two pulling ropes for controlling releasing is a circle, and the releasing trajectory is located on the plane where the central axis of the rocket and the plug are located.

3. A secondary thrust-off device for rocket launchers as claimed in claim 1, further comprising: the traction rope is recovered, and the driving part is provided with a second winding drum;

Two ends of the recovery pulling rope are respectively connected with the release plug and the second winding drum;

the driving component drives the recovery pulling rope to recover on the second winding drum after being started in the forward direction, and the recovery pulling rope is used for exerting upward acting force on the release plug in the falling process after the release plug and the plug are separated.

4. An auxiliary releasing device for rocket launcher according to claim 3, wherein said driving means is actuated in reverse to extend said release pull string and said recovery pull string in the case where said erector is tilted from horizontal with respect to the rocket body of said rocket before said rocket is launched.

5. An auxiliary pulling device for a rocket launcher according to claim 3, wherein said first reel has a first distance from said release insert and said second reel has a second distance from said release insert, said first distance being less than said second distance.

6. An auxiliary pulling apparatus for a rocket launcher according to claim 3, wherein said driving means comprises a primary driving member and a backup driving member;

in the event of a failure of the primary drive, the backup drive is enabled.

7. An auxiliary pulling device for a rocket launcher according to claim 3, wherein the range of the angle a at which said erector is inclined with respect to the rocket body of said rocket includes: a is more than or equal to 15 degrees and more than or equal to 9 degrees;

the separation pulling force applied by the separation pulling rope to the disengaging and inserting has a first direction, the extension line of the central axis of the plug and the disengaging and inserting is a disengaging and inserting axis, and the angle deviation between the first direction and the disengaging and inserting axis is less than 5 degrees;

when the plug and the socket are connected, the angular deviation between the cable and the plug axis is 40 degrees or less.

8. A secondary thrust device for rocket launchers according to claim 3, wherein said secondary thrust device for rocket launchers further comprises: the fixing plate, the first guide piece, the second guide piece and the third guide piece;

the fixed plate is close to the driving part, the fixed plate is arranged on the erecting frame, and the guide piece is arranged on the fixed plate;

the separation pulling rope is wound on the first guide member after being stretched; the recovery traction rope is wound on the second guide member after being stretched; the cable is wound around the third guide before the rising frame is tilted.

9. An auxiliary pulling-off device for a rocket launcher according to claim 8, wherein the number of said first guide, said second guide, and said third guide is one or more than two;

one end of the separation pulling rope is connected with the first winding drum after passing through one or more than two first guide pieces, and one end of the recovery pulling rope is connected with the second winding drum after passing through one or more than two second guide pieces; one end of the cable passes through one or more than two third guiding pieces and then is connected with the plug-in and plug-out device.